Static Aerodynamic Characteristics Of A Short Blunt 10 Degree Semivertex Angle Cone At A Mach Number Of 15 In Helium
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Author |
: Melvin J. Fohrman |
Publisher |
: |
Total Pages |
: 48 |
Release |
: 1963 |
ISBN-10 |
: UIUC:30112106874081 |
ISBN-13 |
: |
Rating |
: 4/5 (81 Downloads) |
Synopsis Static Aerodynamic Characteristics of a Short Blunt 10 Degree Semivertex Angle Cone at a Mach Number of 15 in Helium by : Melvin J. Fohrman
Author |
: Melvin J. Fohrman |
Publisher |
: |
Total Pages |
: 37 |
Release |
: 1963 |
ISBN-10 |
: OCLC:761406244 |
ISBN-13 |
: |
Rating |
: 4/5 (44 Downloads) |
Synopsis Static Aerodynamic Characteristics of a Short Blunt 10 Degree Semivertex Angle Cone at a Mach Number of 15 in Helium by : Melvin J. Fohrman
Author |
: J. Wayne Keyes |
Publisher |
: |
Total Pages |
: 72 |
Release |
: 1964 |
ISBN-10 |
: UIUC:30112106866558 |
ISBN-13 |
: |
Rating |
: 4/5 (58 Downloads) |
Synopsis Longitudinal Aerodynamic Characteristics of Blunted Cones at Mach Numbers of 3.5, 4.2, and 6.0 by : J. Wayne Keyes
Author |
: |
Publisher |
: |
Total Pages |
: 542 |
Release |
: 1964 |
ISBN-10 |
: MINN:31951000845877D |
ISBN-13 |
: |
Rating |
: 4/5 (7D Downloads) |
Synopsis NASA Technical Note by :
Author |
: Stuart L. Treon |
Publisher |
: |
Total Pages |
: 40 |
Release |
: 1961 |
ISBN-10 |
: UIUC:30112106637264 |
ISBN-13 |
: |
Rating |
: 4/5 (64 Downloads) |
Synopsis Static Aerodynamic Characteristics of Short Blunt Cones with Various Nose and Base Cone Angles at Mach Numbers from 0.6 to 5.5 and Angles of Attack to 180 Degrees by : Stuart L. Treon
Author |
: United States. National Aeronautics and Space Administration Scientific and Technical Information Division |
Publisher |
: |
Total Pages |
: 260 |
Release |
: 1964 |
ISBN-10 |
: STANFORD:36105113773431 |
ISBN-13 |
: |
Rating |
: 4/5 (31 Downloads) |
Synopsis NASA Scientific and Technical Reports by : United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Author |
: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division |
Publisher |
: |
Total Pages |
: 258 |
Release |
: 1963 |
ISBN-10 |
: CORNELL:31924004392746 |
ISBN-13 |
: |
Rating |
: 4/5 (46 Downloads) |
Synopsis A Selected Listing of NASA Scientific and Technical Reports for ... by : United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Author |
: |
Publisher |
: |
Total Pages |
: 296 |
Release |
: 1991 |
ISBN-10 |
: MINN:31951P00218510W |
ISBN-13 |
: |
Rating |
: 4/5 (0W Downloads) |
Synopsis NASA Technical Memorandum by :
Author |
: E. L. Clark |
Publisher |
: |
Total Pages |
: 98 |
Release |
: 1964 |
ISBN-10 |
: UOM:39015104951531 |
ISBN-13 |
: |
Rating |
: 4/5 (31 Downloads) |
Synopsis Equations and Charts for the Evaluation of the Hypersonic Aerodynamic Characteristics of Lifting Configurations by the Newtonian Theory by : E. L. Clark
The pressure distribution predicted by the modified Newtonian theory is used to develop equations for the aerodynamic forces, moments, and stability derivatives for components of hypersonic lifting configurations. In conjunction with the equations, a set of charts is presented to enable simple determination of the aerodynamic characteristics of swept cylinders, swept wedges, spherical segments, and cone frustums at zero sideslip and angles of attack from 0 to 180 degrees. This method allows evaluation of most delta wing-body combinations without the need for numerical or graphical integration. As an example of the procedure, the theoretical characteristics of a blunt 75-degree swept delta wing are calculated and compared with experimental results.
Author |
: Stuart L. Treon |
Publisher |
: |
Total Pages |
: 35 |
Release |
: 1962 |
ISBN-10 |
: OCLC:760990895 |
ISBN-13 |
: |
Rating |
: 4/5 (95 Downloads) |
Synopsis Static Aerodynamic Characteristics of Short Blunt Cones with Various Nose and Base Cone Angles at Mach Numbers from 0.6 to 5.5 and Angles of Attack to 180 Degrees by : Stuart L. Treon